The aerodynamic forces on any control surface produce a moment about the hinge.
在任何操纵面上的空气动力均产生围绕其铰链轴的力矩。
The control moment from control law is allocated to aero-surface and reaction control system, in this phase the limits from hardware are taken into consideration.
将控制律给出的控制力矩合理分配给气动面的反作用控制系统，并考虑了实际的硬件特性要求。
To a certain type of aircraft, for example, describes the process in detail how to use the methods to measure hinge moment of control surface.
以某型飞机为例，详细描述了如何利用该方法测量舵面铰链力矩的过程。
To a certain type of aircraft, for example, describes the process in detail how to use the methods to measure hinge moment of control surface.
以某型飞机为例，详细描述了如何利用该方法测量舵面铰链力矩的过程。
应用推荐